[1] Persovaa M G, Soloveichika Y G, Belovb V K. Modeling of aerodynamic heat flux and thermoelastic behavior of nose caps of hypersonic vehicles [J].Acta Astronautica, 2017, 136(1): 312-331. [2] 张志豪, 孙得川.飞行器气动加热烧蚀工程计算[J]. 兵工学报, 2015, 36(10): 1949-1954. ZHANG Zhi-hao, SUN De-chuan. Calculation of aerodynamic heating and ablation of multi-layer thermal protection material[J]. Acta Armamentarii, 2015, 36(10): 1949-1954. (in Chinese) [3] 童福林, 李新亮, 唐志共, 等. 转捩对压缩拐角激波/边界层干扰分离泡的影响[J]. 航空学报, 2016, 37(10): 2909-2912. TONG Fu-lin, LI Xin-liang, TANG Zhi-gong, et al. Transition effect on separation bubble of shock wave/boundary layer interaction in a compression ramp[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(10): 2909-2912. (in Chinese) [4] 宋友富, 徐晶磊, 张杨, 等. 压缩拐角激波/边界层干扰的可压缩湍流模型研究[J]. 推进技术, 2017, 38(2): 281-288. SONG Yong-fu, XU Jing-lei, ZHANG Yang, et al. Research of compressible trubulence model in shock wave/boundary-layer interaction flow at a compression corner[J]. Journal of Propulsion Technology, 2017, 38(2): 281-288. (in Chinese) [5] 董祥瑞, 陈耀慧, 董刚, 等. 基于双微楔的高超声速激波与边界层干扰控制研究[J]. 兵工学报, 2016, 37(9): 1624-1632. DONG Xiang-rui, CHEN Yao-hui, DONG Gang, et al. Research on control of hypersonic shock wave/boundary layer interactions by double micro-ramps[J]. Acta Armamentarii, 2016, 37(9): 1624-1632. (in Chinese) [6] Bisek N J. High-fidelity simulations of the HIFiRE-6 flow path, AIAA-2016-1115[R]. Reston, VA, US: AIAA, 2016. [7] Kimmel R L, Adamczak D W. HIFiRE-1 flight trajectory estimation and initial experimental results, AIAA-2011-2358 [R]. Reston, VA, US: AIAA, 2011. [8] MacLean M, Wadhams T, Holden M, et al. Ground test studies of the HIFiRE-1 transition experiment—part 2: computational analysis[J]. Journal of Spacecraft and Rockets, 2008, 45(6): 1149- 1164. [9] Wadhams T, Mundy E, MacLean M, et al. Pre-flight ground testing of the full-scale HIFiRE-1vehicle at fully duplicated flight conditions: part II, AIAA-2008-0639[R]. Reston, VA, US: AIAA, 2008. [10] Kimmel R L, Adamczak D W. HIFiRE-1 preliminary aerothermodynamics measurements, AIAA-2011-3413[R]. Reston, VA, US: AIAA, 2011.
[11] Stanfield S A, Kimmel R L, Adamczak D W, et al. Boundary layer transition experiment during reentry of HIFiRE-1[J]. Journal of Spacecraft and Rockets, 2015, 52(3): 637-649. [12] Yentsch R J, Gaitonde D V, Kimmel R L. Performance of turbulence modeling in simulation of the HIFiRE-1 flight test[J]. Journal of Spacecraft and Rockets, 2014, 51(1): 117-127. [13] Rautaheimo P R. Developments in turbulence modeling with Reynolds-averaged Navie Stokes equations[M]. Helsinki, Finland: Finnish Academies Technology Press, 2001: 17-19. [14] Xu L, Wu Q J, Weng P F. HLLC Riemann solver based on high-order reconstruction for unsteady inviscid compressible flows[C]∥Proceedings of IEEE International Conference on Computer Science and Automation Engineering. Shanghai, China: IEEE, 2011: 618-622. [15] Holden M, Wadhams T, MacLean M, et al. Experimental studies of shock wave/turbulent boundary layer interaction in high Reynolds number supersonic and hypersonic flows to evaluate the performance of CFD codes, AIAA-2010-4468[R]. Reston, VA, US: AIAA, 2010. [16] Yang J L, Liu M. A wall grid scale criterion for hypersonic aerodynamic heating calculation[J]. Acta Astronautica, 2017, 136(1): 137-143. [17] 张智超, 高振勋, 蒋崇文, 等. 高超声速气动热数值计算壁面网格准则[J]. 北京航空航天大学学报, 2015, 41(4): 594-600. ZHANG Zhi-chao, GAO Zhen-xun, JIANG Chong-wen, et al. Grid generation criterions in hypersonic aeroheating computations[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(4): 594-600. (in Chinese) [18] Sohag F A, Mohanta L, Cheung F B. CFD analyses of mixed and forced convection in a heated vertical rod bundle[J]. Applied Thermal Engineering, 2017, 117(4): 85-93.
第39卷 第3期2018 年3月兵工学报ACTA ARMAMENTARIIVol.39No.3Mar.2018
|